US20030189028A1 - Apparatus and method for forming a body - Google Patents
Apparatus and method for forming a body Download PDFInfo
- Publication number
- US20030189028A1 US20030189028A1 US10/406,265 US40626503A US2003189028A1 US 20030189028 A1 US20030189028 A1 US 20030189028A1 US 40626503 A US40626503 A US 40626503A US 2003189028 A1 US2003189028 A1 US 2003189028A1
- Authority
- US
- United States
- Prior art keywords
- wall
- welding head
- support member
- formation
- manipulating
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 238000000034 method Methods 0.000 title claims abstract description 38
- 238000003466 welding Methods 0.000 claims abstract description 78
- 239000000463 material Substances 0.000 claims abstract description 36
- 230000008021 deposition Effects 0.000 claims abstract description 7
- 230000005611 electricity Effects 0.000 claims abstract description 6
- 238000005304 joining Methods 0.000 claims abstract description 6
- 230000015572 biosynthetic process Effects 0.000 claims description 20
- 238000011960 computer-aided design Methods 0.000 claims description 2
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 12
- 229910052751 metal Inorganic materials 0.000 description 12
- 239000002184 metal Substances 0.000 description 12
- 239000011261 inert gas Substances 0.000 description 8
- 229910052786 argon Inorganic materials 0.000 description 6
- 239000007789 gas Substances 0.000 description 5
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 description 5
- 239000000758 substrate Substances 0.000 description 5
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 2
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 2
- 229910052721 tungsten Inorganic materials 0.000 description 2
- 239000010937 tungsten Substances 0.000 description 2
- 229910001069 Ti alloy Inorganic materials 0.000 description 1
- 239000004411 aluminium Substances 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910002092 carbon dioxide Inorganic materials 0.000 description 1
- 239000001569 carbon dioxide Substances 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K9/00—Arc welding or cutting
- B23K9/04—Welding for other purposes than joining, e.g. built-up welding
- B23K9/044—Built-up welding on three-dimensional surfaces
- B23K9/046—Built-up welding on three-dimensional surfaces on surfaces of revolution
- B23K9/048—Built-up welding on three-dimensional surfaces on surfaces of revolution on cylindrical surfaces
Definitions
- This invention relates to an apparatus and method for forming a body by deposition of a weld material.
- the formation of components for aerospace engines can be carried out by any of several techniques involving deposition of a weld material.
- These techniques utilise an apparatus including two electrodes, the first electrode being held in a welding head to which is fed a supply of a metal wire constituting the weld material.
- the second electrode is in the form of a substrate or foundation upon which the weld material is to be deposited to form the component.
- the foundation may be in the form of a metal plate.
- a supply of an inert gas is fed to the welding head during its operation.
- the welding head and the foundation are connected to a supply of electricity, an arc is formed in the inert gas which melts the metal wire and a small region of the material forming the foundation.
- the metal is then deposited onto the foundation in a controlled manner.
- the welding head is mounted on a robotic arm and the foundation is mounted on a movable turntable. By controlling the movement of the arm and the turntable, the metal can be deposited on the foundation in order to form components of any desired shape.
- One such method of forming components involves providing the welding head with a permanent electrode and also providing a separate metal wire to the welding head, the metal wire constituting the weld material.
- This method is generally known in the art as tungsten inert gas welding which is generally shortened to TIG welding. Although tungsten is commonly used, it will be appreciated by those skilled in the art that other suitable materials could be used as the electrode.
- Another such method involves the use of a sacrificial electrode in the welding head. With this arrangement, the metal wire which provides the weld material also constitutes the electrode and is fed through the welding head. This method is generally known in the art as metal inert gas welding, which is generally shortened to MIG welding.
- a method of forming a body by deposition of a weld material including the steps of:
- Each wall may be axi-symmetrical.
- the first wall may be substantially cylindrical.
- the second and third walls may be generally frustoconical.
- the hollow section body may be generally annular.
- the hollow section body may be for forming part of a casing structure for a gas turbine engine.
- the electrical supply is controlled such that during the formation of each wall, the current is higher during the formation of a proximal base part of the wall than it is during the formation of a mid part of the wall, such that the base part of the wall is broader than the mid part of the wall.
- the electrical supply is controlled such that during the formation of each wall, the current is higher when forming a distal part of the wall than when forming the mid part of the wall, such that the distal part of the wall is broader than the mid part of the wall.
- the support member is oriented substantially horizontally and the welding head substantially vertically, such that a substantially vertical first wall is produced.
- the support member is tilted to an angle of between 10° and 50° to the horizontal.
- the second wall may then be deposited onto the first wall at an angle thereto.
- the support member and the welding head may be manipulated such that the first wall is held at an angle to the horizontal and the second wall is built up on the first wall.
- the second wall may be built up substantially vertically.
- the support member may be manipulated such that the second wall is angled to the vertical.
- the first wall may be substantially horizontal.
- the support member and the welding head may then be manipulated to form the third wall, joining the first and second walls.
- the method may include the step of further producing fourth and optionally subsequent walls, the walls together forming a hollow section body.
- the welding head may initially be oriented substantially vertically. As the wall is built up, the orientation of the head may be gradually altered such that its angle to the vertical gradually increases.
- the method may include the steps of:
- the method includes the use of a robot for manipulating the welding head, the robot preferably having six degrees of freedom of movement.
- FIG. 1 is a diagrammatic side view of apparatus for forming a body
- FIGS. 2 A to 2 C are diagrammatic illustrations of a process for forming a body
- FIG. 3 is a diagrammatic illustration showing the formation of the final wall of the body.
- FIG. 1 there is shown an apparatus 10 for forming a body by deposition of a weld material.
- the apparatus 10 includes an arc welding head 12 , mounted on a free end of a support mechanism in the form of a robot arm 14 .
- the robot arm 14 includes a base member 16 on which are pivotally mounted a plurality of sections 18 which are rotatable relative to one another and about their own axes so that the welding head 12 can be manipulated to any desired position.
- the welding head 12 includes a first electrode 19 .
- a supply of a metal wire 24 is provided, in the form of a reel 22 around which the wire 24 is wound.
- the metal is in the form of a titanium alloy, for example titanium 6 / 4 which includes 6% aluminium and 4% vanadium.
- the wire 24 is fed from the reel 22 to the welding head 12 such that an end of the wire 24 is held just below the tip of the welding head 12 .
- the wire 24 is held in place by suitable holding means 26 .
- the apparatus 10 also includes a supply of an inert gas, stored in a cylinder 28 .
- a pipe 30 leads from the cylinder 28 to the welding head 12 through the sections 18 .
- the gas is any suitable inert gas or gases or combinations of inert and active gases, for example argon or argon/carbon dioxide, and provides the medium in which an arc is formed, as will be explained below.
- Support means 34 is provided beneath the welding head 12 and includes a turntable 36 mounted upon a platform 38 .
- the platform 38 is pivotally mounted as indicated by the arrow A, by pivot 40 , to a pedestal 42 which in turn is rotatably mounted, as indicated by the arrow B, upon a base member 44 .
- Control means in the form of a computer 46 controls the movement of the support means 34 and the robot arm 14 , as well as controlling the supply of the inert gas, and the supply of the metal wire 24 .
- the turntable 36 and the welding head 12 are connected to a supply of electricity, and argon is fed via the pipe 30 from the cylinder 28 to the welding head 12 to form an argon shroud around the electrode of the welding head 12 .
- the argon shroud extends to the substrate on which material is to be deposited (i.e. the support member or the part of the body being worked upon).
- the argon gas is ionised to form a plasma and an arc is created between the first electrode 19 in the welding head 12 and the substrate.
- the arc produces a high temperature, which is sufficient to melt the material of the substrate in the vicinity of the arc and to melt the end of the wire 24 which is also in the vicinity of the arc. This melted material from the wire 24 and the foundation plate 52 forms a molten weld pool.
- the position of the welding head 12 relative to the turntable 36 is controlled by the computer 46 by manipulating both the position of the welding head 12 , and the position of the turntable 36 .
- the computer 46 also controls the rate of feeding of the wire 24 .
- a component for example for use in a gas turbine engine, can be built up layer by layer by the deposition of the weld material from the wire 24 .
- the welding head 12 deposits material on the body rather than the support member.
- the shroud extends from the welding head 12 to the part of the body being formed and the arc is created between the welding head 12 and the body.
- substrate is intended to cover either the support member or the body as appropriate.
- FIGS. 2A to 2 C and FIG. 3 there is illustrated a method of forming a hollow section body.
- the turntable 36 and the robot arm 14 are manipulated such that the turntable 36 is located substantially horizontally and the welding head 12 on the robot arm 14 is oriented substantially vertically.
- the welding head 12 and the turntable 36 are both connected to a supply of electricity and the turntable 36 rotated together with the welding head being raised, to form a generally cylindrical first wall, 40 , layer by layer.
- the turntable 36 is then tilted, such that the cylindrical first wall 40 is angled to the vertical.
- the welding head 12 is then manipulated to form a frustoconical second wall 42 , angled to the first wall.
- the turntable 36 is again rotated so that the second wall extends all around the first.
- the turntable 36 is again manipulated such that the substantially cylindrical first wall 40 is oriented generally with its axis horizontally.
- the second wall 42 is thus at an angle of say 20° to 30° to the vertical.
- the robot arm 14 and the welding head 12 are then manipulated to form a frustoconical third wall 44 , joining the first two walls 40 and 42 and forming a closed triangular section body.
- the welding head 12 is oriented substantially vertically. As the welding head 12 is raised to form the wall 44 , its angle to the vertical is gradually increased until it is eventually angled at about 20° to 30° to the vertical.
- the current is set to be relatively high. This causes the formation of a relatively large weld pool and thus a thick wall as may be seen in FIG. 3. As the welding head is raised towards the mid point of each wall, the current is reduced thus reducing the width of the wall. By having a relatively thick portion at the base of each wall, the heat may be effectively dissipated and the joins between adjacent walls tends to be smooth and include no sharp edges. The current is again increased towards the distal ends of each wall and this, together with the angle of the welding head, ensures that the walls join smoothly and in a curved manner.
- the above hollow, triangular sections may be used to stiffen casings, in particular the inner case of a jet engine.
Abstract
Description
- This invention relates to an apparatus and method for forming a body by deposition of a weld material.
- The formation of components for aerospace engines can be carried out by any of several techniques involving deposition of a weld material. These techniques utilise an apparatus including two electrodes, the first electrode being held in a welding head to which is fed a supply of a metal wire constituting the weld material. The second electrode is in the form of a substrate or foundation upon which the weld material is to be deposited to form the component. The foundation may be in the form of a metal plate. A supply of an inert gas is fed to the welding head during its operation.
- When the welding head and the foundation are connected to a supply of electricity, an arc is formed in the inert gas which melts the metal wire and a small region of the material forming the foundation. The metal is then deposited onto the foundation in a controlled manner. The welding head is mounted on a robotic arm and the foundation is mounted on a movable turntable. By controlling the movement of the arm and the turntable, the metal can be deposited on the foundation in order to form components of any desired shape.
- One such method of forming components involves providing the welding head with a permanent electrode and also providing a separate metal wire to the welding head, the metal wire constituting the weld material. This method is generally known in the art as tungsten inert gas welding which is generally shortened to TIG welding. Although tungsten is commonly used, it will be appreciated by those skilled in the art that other suitable materials could be used as the electrode.
- Another such method involves the use of a sacrificial electrode in the welding head. With this arrangement, the metal wire which provides the weld material also constitutes the electrode and is fed through the welding head. This method is generally known in the art as metal inert gas welding, which is generally shortened to MIG welding.
- According to the invention there is provided a method of forming a body by deposition of a weld material, the method including the steps of:
- providing a welding head;
- providing a support member upon which the body is to be formed;
- supplying a weld material to the welding head, the weld material to be deposited on the support member; and
- connecting the support member and the welding head to a supply of electricity to form an arc between the welding head and the support member or the body to melt the material, the method further including the steps of:
- manipulating the support member and the welding head relative to one another to deposit material to form a first wall;
- manipulating the support member and the welding head relative to one another to deposit material to form a second wall extending from and angled to the first wall; and
- manipulating the support member and the welding head relative to one another to deposit material to form a third wall joining the first two walls to form a hollow section body.
- Each wall may be axi-symmetrical. The first wall may be substantially cylindrical. The second and third walls may be generally frustoconical. The hollow section body may be generally annular. The hollow section body may be for forming part of a casing structure for a gas turbine engine.
- Preferably the electrical supply is controlled such that during the formation of each wall, the current is higher during the formation of a proximal base part of the wall than it is during the formation of a mid part of the wall, such that the base part of the wall is broader than the mid part of the wall.
- Preferably the electrical supply is controlled such that during the formation of each wall, the current is higher when forming a distal part of the wall than when forming the mid part of the wall, such that the distal part of the wall is broader than the mid part of the wall.
- Preferably during the formation of the first wall, the support member is oriented substantially horizontally and the welding head substantially vertically, such that a substantially vertical first wall is produced.
- Following the formation of the first wall, preferably the support member is tilted to an angle of between 10° and 50° to the horizontal. The second wall may then be deposited onto the first wall at an angle thereto. The support member and the welding head may be manipulated such that the first wall is held at an angle to the horizontal and the second wall is built up on the first wall. The second wall may be built up substantially vertically.
- Following formation of the second wall, the support member may be manipulated such that the second wall is angled to the vertical. The first wall may be substantially horizontal. The support member and the welding head may then be manipulated to form the third wall, joining the first and second walls.
- The method may include the step of further producing fourth and optionally subsequent walls, the walls together forming a hollow section body.
- During the formation of an angled wall, the welding head may initially be oriented substantially vertically. As the wall is built up, the orientation of the head may be gradually altered such that its angle to the vertical gradually increases.
- The method may include the steps of:
- initially producing a two or three dimensional model of the body to be formed, using computer aided design and computer aided manufacturing software;
- taking into account the geometry of the support member and of the means for manipulating the welding head, producing a defined path for the welding head to follow;
- using the above information to produce a welding program in which each positionable point for the welding head is defined; and
- utilising the above program to control the means for manipulating the welding head.
- Preferably the method includes the use of a robot for manipulating the welding head, the robot preferably having six degrees of freedom of movement.
- An embodiment of the invention will now be described for the purpose of illustration only with reference to the accompanying drawings in which:
- FIG. 1 is a diagrammatic side view of apparatus for forming a body;
- FIGSs.2A to 2C are diagrammatic illustrations of a process for forming a body; and
- FIG. 3 is a diagrammatic illustration showing the formation of the final wall of the body.
- Referring to FIG. 1, there is shown an
apparatus 10 for forming a body by deposition of a weld material. Theapparatus 10 includes anarc welding head 12, mounted on a free end of a support mechanism in the form of arobot arm 14. Therobot arm 14 includes abase member 16 on which are pivotally mounted a plurality ofsections 18 which are rotatable relative to one another and about their own axes so that thewelding head 12 can be manipulated to any desired position. Thewelding head 12 includes afirst electrode 19. - A supply of a
metal wire 24 is provided, in the form of areel 22 around which thewire 24 is wound. The metal is in the form of a titanium alloy, for example titanium 6/4 which includes 6% aluminium and 4% vanadium. Thewire 24 is fed from thereel 22 to thewelding head 12 such that an end of thewire 24 is held just below the tip of thewelding head 12. Thewire 24 is held in place bysuitable holding means 26. - The
apparatus 10 also includes a supply of an inert gas, stored in acylinder 28. Apipe 30 leads from thecylinder 28 to thewelding head 12 through thesections 18. The gas is any suitable inert gas or gases or combinations of inert and active gases, for example argon or argon/carbon dioxide, and provides the medium in which an arc is formed, as will be explained below. - Support means34 is provided beneath the
welding head 12 and includes aturntable 36 mounted upon aplatform 38. Theplatform 38 is pivotally mounted as indicated by the arrow A, bypivot 40, to apedestal 42 which in turn is rotatably mounted, as indicated by the arrow B, upon abase member 44. - Control means in the form of a
computer 46 controls the movement of the support means 34 and therobot arm 14, as well as controlling the supply of the inert gas, and the supply of themetal wire 24. - In operation, the
turntable 36 and thewelding head 12 are connected to a supply of electricity, and argon is fed via thepipe 30 from thecylinder 28 to thewelding head 12 to form an argon shroud around the electrode of thewelding head 12. The argon shroud extends to the substrate on which material is to be deposited (i.e. the support member or the part of the body being worked upon). The argon gas is ionised to form a plasma and an arc is created between thefirst electrode 19 in thewelding head 12 and the substrate. The arc produces a high temperature, which is sufficient to melt the material of the substrate in the vicinity of the arc and to melt the end of thewire 24 which is also in the vicinity of the arc. This melted material from thewire 24 and the foundation plate 52 forms a molten weld pool. - The position of the
welding head 12 relative to theturntable 36 is controlled by thecomputer 46 by manipulating both the position of thewelding head 12, and the position of theturntable 36. Thecomputer 46 also controls the rate of feeding of thewire 24. Thus, by appropriate manipulation of thewelding head 12 relative to theturntable 36, a component, for example for use in a gas turbine engine, can be built up layer by layer by the deposition of the weld material from thewire 24. As will be appreciated when the body is partially formed, thewelding head 12 deposits material on the body rather than the support member. In this case, the shroud extends from thewelding head 12 to the part of the body being formed and the arc is created between the weldinghead 12 and the body. The term “substrate” is intended to cover either the support member or the body as appropriate. - Referring to FIGS. 2A to2C and FIG. 3, there is illustrated a method of forming a hollow section body.
- Referring to FIG. 2A, in a first step, the
turntable 36 and therobot arm 14 are manipulated such that theturntable 36 is located substantially horizontally and thewelding head 12 on therobot arm 14 is oriented substantially vertically. Thewelding head 12 and theturntable 36 are both connected to a supply of electricity and theturntable 36 rotated together with the welding head being raised, to form a generally cylindrical first wall, 40, layer by layer. - Referring to FIG. 2B, the
turntable 36 is then tilted, such that the cylindricalfirst wall 40 is angled to the vertical. Thewelding head 12 is then manipulated to form a frustoconicalsecond wall 42, angled to the first wall. Theturntable 36 is again rotated so that the second wall extends all around the first. - Referring to FIGS. 2C and 3, the
turntable 36 is again manipulated such that the substantially cylindricalfirst wall 40 is oriented generally with its axis horizontally. Thesecond wall 42 is thus at an angle of say 20° to 30° to the vertical. Therobot arm 14 and thewelding head 12 are then manipulated to form a frustoconicalthird wall 44, joining the first twowalls - Referring to FIG. 3, it may be seen that initially the
welding head 12 is oriented substantially vertically. As thewelding head 12 is raised to form thewall 44, its angle to the vertical is gradually increased until it is eventually angled at about 20° to 30° to the vertical. - When the welding head is at the base of a wall, starting to form the wall, the current is set to be relatively high. This causes the formation of a relatively large weld pool and thus a thick wall as may be seen in FIG. 3. As the welding head is raised towards the mid point of each wall, the current is reduced thus reducing the width of the wall. By having a relatively thick portion at the base of each wall, the heat may be effectively dissipated and the joins between adjacent walls tends to be smooth and include no sharp edges. The current is again increased towards the distal ends of each wall and this, together with the angle of the welding head, ensures that the walls join smoothly and in a curved manner.
- There is thus provided a method for providing hollow structures. Whereas in prior art methods such as casting, there is a need for holes in such hollow structures, the above method enables the formation of truly hollow, enclosed shapes. This improves the structural integrity of the body.
- The above hollow, triangular sections may be used to stiffen casings, in particular the inner case of a jet engine.
- Various modifications may be made to the above described embodiment without departing from the scope of the invention. In particular, the exact orientations of the support member and the welding head will depend upon the shape of material to be formed and is not fixed. However, the person skilled in the art will be able to determine suitable orientations in each case.
- Whilst endeavouring in the foregoing specification to draw attention to those features of the invention believed to be of particular importance it should be understood that the Applicant claims protection in respect of any patentable feature or combination of features hereinbefore referred to and/or shown in the drawings whether or not particular emphasis has been placed thereon.
Claims (12)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
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GB0208226 | 2002-04-09 | ||
GBGB0208226.1A GB0208226D0 (en) | 2002-04-09 | 2002-04-09 | Apparatus and method for forming a body |
GB0208226.1 | 2002-04-09 |
Publications (2)
Publication Number | Publication Date |
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US20030189028A1 true US20030189028A1 (en) | 2003-10-09 |
US6825433B2 US6825433B2 (en) | 2004-11-30 |
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US10/406,265 Expired - Lifetime US6825433B2 (en) | 2002-04-09 | 2003-04-04 | Apparatus and method for forming a body |
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EP (1) | EP1354658A3 (en) |
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Cited By (9)
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US20090277877A1 (en) * | 2008-05-08 | 2009-11-12 | Daniels Craig A | Apparatus and method for welding objects |
US20120328902A1 (en) * | 2011-06-22 | 2012-12-27 | General Electric Company | Method of fabricating a component and a manufactured component |
US8678805B2 (en) | 2008-12-22 | 2014-03-25 | Dsm Ip Assets Bv | System and method for layerwise production of a tangible object |
US20140093368A1 (en) * | 2012-09-28 | 2014-04-03 | United Technologies Corporation | Outer case with gusseted boss |
US8777602B2 (en) | 2008-12-22 | 2014-07-15 | Nederlandse Organisatie Voor Tobgepast-Natuurwetenschappelijk Onderzoek TNO | Method and apparatus for layerwise production of a 3D object |
US8905739B2 (en) | 2008-12-22 | 2014-12-09 | Nederlandse Organisatie Voor Toegepast-Natuurwetenschappelijk Onderzoek Tno | Method and apparatus for layerwise production of a 3D object |
US9938834B2 (en) | 2015-04-30 | 2018-04-10 | Honeywell International Inc. | Bladed gas turbine engine rotors having deposited transition rings and methods for the manufacture thereof |
US10036254B2 (en) | 2015-11-12 | 2018-07-31 | Honeywell International Inc. | Dual alloy bladed rotors suitable for usage in gas turbine engines and methods for the manufacture thereof |
US10294804B2 (en) | 2015-08-11 | 2019-05-21 | Honeywell International Inc. | Dual alloy gas turbine engine rotors and methods for the manufacture thereof |
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CA2629041A1 (en) * | 2008-04-14 | 2009-10-14 | Steven L. Pankhurst | Weld-on-weld device |
AT506217B1 (en) * | 2008-05-28 | 2009-07-15 | Fronius Int Gmbh | METHOD FOR PRODUCING A STRUCTURE ON A SURFACE OF A METALLIC WORKPIECE |
FR2931714B1 (en) * | 2008-05-30 | 2010-06-25 | Snecma | CONSTRUCTION OF A PART OF A METAL PIECE BY THE MIG PROCESS WITH CURRENT AND PULSED WIRE |
US20110156304A1 (en) * | 2009-12-31 | 2011-06-30 | Bryant Walker | Die Tool Production Methods Utilizing Additive Manufacturing Techniques |
CN103801799B (en) | 2012-11-12 | 2017-11-21 | 通用电气公司 | The revolving meber for manufacturing the method for revolving meber and being manufactured with this method |
US20160221122A1 (en) * | 2015-02-03 | 2016-08-04 | Hamilton Sundstrand Corporation | Hybrid additive manufacturing method for rotor |
RU193110U1 (en) * | 2019-06-13 | 2019-10-15 | Федеральное государственное бюджетное образовательное учреждение высшего образования "Тверской государственный технический университет" (ТвГТУ) | Automatic installation for 3D printing of metal products of complex shape |
RU198092U1 (en) * | 2020-01-09 | 2020-06-17 | Федеральное государственное бюджетное образовательное учреждение высшего образования "Тверской государственный технический университет" | Installation for 3D printing of metal products |
JP2021130130A (en) * | 2020-02-21 | 2021-09-09 | 三菱重工コンプレッサ株式会社 | Metal laminate shaping method |
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- 2002-04-09 GB GBGB0208226.1A patent/GB0208226D0/en not_active Ceased
-
2003
- 2003-03-19 EP EP03251713A patent/EP1354658A3/en not_active Withdrawn
- 2003-04-04 US US10/406,265 patent/US6825433B2/en not_active Expired - Lifetime
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Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
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US20090277877A1 (en) * | 2008-05-08 | 2009-11-12 | Daniels Craig A | Apparatus and method for welding objects |
US8678805B2 (en) | 2008-12-22 | 2014-03-25 | Dsm Ip Assets Bv | System and method for layerwise production of a tangible object |
US8777602B2 (en) | 2008-12-22 | 2014-07-15 | Nederlandse Organisatie Voor Tobgepast-Natuurwetenschappelijk Onderzoek TNO | Method and apparatus for layerwise production of a 3D object |
US8905739B2 (en) | 2008-12-22 | 2014-12-09 | Nederlandse Organisatie Voor Toegepast-Natuurwetenschappelijk Onderzoek Tno | Method and apparatus for layerwise production of a 3D object |
US20120328902A1 (en) * | 2011-06-22 | 2012-12-27 | General Electric Company | Method of fabricating a component and a manufactured component |
US8921730B2 (en) * | 2011-06-22 | 2014-12-30 | General Electric Company | Method of fabricating a component and a manufactured component |
US20140093368A1 (en) * | 2012-09-28 | 2014-04-03 | United Technologies Corporation | Outer case with gusseted boss |
US9328629B2 (en) * | 2012-09-28 | 2016-05-03 | United Technologies Corporation | Outer case with gusseted boss |
US9938834B2 (en) | 2015-04-30 | 2018-04-10 | Honeywell International Inc. | Bladed gas turbine engine rotors having deposited transition rings and methods for the manufacture thereof |
US10294804B2 (en) | 2015-08-11 | 2019-05-21 | Honeywell International Inc. | Dual alloy gas turbine engine rotors and methods for the manufacture thereof |
US10036254B2 (en) | 2015-11-12 | 2018-07-31 | Honeywell International Inc. | Dual alloy bladed rotors suitable for usage in gas turbine engines and methods for the manufacture thereof |
Also Published As
Publication number | Publication date |
---|---|
EP1354658A3 (en) | 2004-11-03 |
EP1354658A2 (en) | 2003-10-22 |
GB0208226D0 (en) | 2002-05-22 |
US6825433B2 (en) | 2004-11-30 |
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